# Service difficulty reports: N660CP

A list on [N660CP](https://openairdocs.org/aircraft/N660CP.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SROM20200810002](https://openairdocs.org/sdr/SROM20200810002.md): Skin · cracked · Aug 10, 2020 · N660CP · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > TWO CRACKS IN LT HORIZONTAL STABILIZER LOWER SKIN, HSS 157, 9 AND 16 FROM THE AFT SPAR. REPAIRED THE SKIN IAW SRM 55-10-01-2R-11, REV 70.
- [SDR SROM20200810001](https://openairdocs.org/sdr/SROM20200810001.md): Skin · cracked · Aug 10, 2020 · N660CP · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > CRACK IN LH HORIZONTAL STABILIZER LOWER SKIN, STAB STA. 101, 19” FORM THE FORWARD SPAR. REPAIRED CRACK IN LH HORIZONTAL STABILIZER LOWER SKIN AT STA. 101, 19” FROM THE FORWARD SPAR IN ACCORDANCE WITH B737-700 SRM 55-10-01-2R-11 REV. 70.
- [SDR SROM2020051300000](https://openairdocs.org/sdr/SROM2020051300000.md): Battery Pack · discharged · May 13, 2020 · N660CP · Boeing 7377BD · Emergency Lighting
  > EMERGENCY LIGHTS ROW 14 AND 16 AIRCRAFT LEFT INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK AT ROW 14 AND 16 LH IAW B737-700 AMM 33-51-00. OPS CHECK OK.
- [SDR 2019FA0000385](https://openairdocs.org/sdr/2019FA0000385.md): Battery Pack · discharged · Nov 26, 2019 · N660CP · Boeing 7377BD · Emergency Lighting
  > RH OVERWING EMERGENCY LIGHTS INOP.
- [SDR SROM2019F00225](https://openairdocs.org/sdr/SROM2019F00225.md): Battery · discharged · Jul 1, 2019 · N660CP · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT SIGN/LIGHT AT LH OVERWING EXIT WILL NOT STAY LIT.
- [SDR 2016F00108](https://openairdocs.org/sdr/2016F00108.md): Frame · dented · Apr 26, 2016 · N660CP · Boeing 7377BD · Fuselage Main, Frame
  > INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REQUEST TO ALLOW TO REMAIN IN SERVICE & A R
- [SDR 2016F00111](https://openairdocs.org/sdr/2016F00111.md): Frame · dented · Apr 26, 2016 · N660CP · Boeing 7377BD · Fuselage Main, Frame
  > INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME, PN 146A1285-70, AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REPAIR SCHEME SUGGESTED BY
- [SDR 2016F00113](https://openairdocs.org/sdr/2016F00113.md): Intercostal · deformed · Apr 26, 2016 · N660CP · Boeing 7377BD · Fuselage Miscellaneous Structure
  > DURING INSPECTION, DAMAGE WAS NOTED IN THE UPPER FLANGE OF THE INTERCOSTAL RUNNING BETWEEN BS 787 & BS 807 AT STRINGER 22L. FABRICATED & INSTALLED REPLACEMENT INTERCOSTAL.
- [SDR SROM2016F00098](https://openairdocs.org/sdr/SROM2016F00098.md): Shear Tie · dented · Apr 26, 2016 · N660CP · Boeing 7377BD · Fuselage Internal Mounting Structure
  > INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA AND THERE ARE NOR SRM REPAIRS FOR SHEAR TIE FRAMES.
- [SDR 2016F00110](https://openairdocs.org/sdr/2016F00110.md): Frame · dented · Apr 26, 2016 · N660CP · Boeing 7377BD · Fuselage Main, Frame
  > INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REQUEST TO ALLOW TO CONTINUE IN SERVICE AS
- [SDR SROM2016042600118](https://openairdocs.org/sdr/SROM2016042600118.md): Frame · dented · Apr 26, 2016 · N660CP · Boeing 7377BD · Fuselage Main, Frame
  > INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA AND THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES SO A SERVICE REQUEST WAS RAISED WITH MFG INCLUDING A REQUEST TO ALLOW TO CONTINUE IN S
- [SDR 2016F00109](https://openairdocs.org/sdr/2016F00109.md): Frame · dented · Apr 26, 2016 · N660CP · Boeing 7377BD · Fuselage Main, Frame
  > INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED INCLUDING A REQUEST TO ALLOW TO CONTINUE IN SERVICE AS
- [SDR 2016F00117](https://openairdocs.org/sdr/2016F00117.md): Frame · dented · Apr 26, 2016 · N660CP · Boeing 7377BD · Fuselage Main, Frame
  > INSPECTION REVEALED A DENT IN THE INBD CHORD OF THE FUSELAGE FRAME AT THIS LOCATION. THE SRM ALLOWS NO DENTS IN THIS AREA & THERE ARE NO SRM REPAIRS FOR SHEAR TIED FRAMES, SO A SERVICE REQUEST WAS RAISED, INCLUDING A REPAIR SCHEME SUGGESTED BY ENGINEERING.
- [SDR SROM091220141](https://openairdocs.org/sdr/SROM091220141.md): Warning Light · false activation · Sep 12, 2014 · N660CP · Boeing 7377BD · Door Warning System
  > DURING TAKEOFF ROLL, FORWARD ENTRY DOOR LIGHT ILLUMINATED AT 80 KNOTS. REJECTED TAKEOFF, RETURNED TO GATE. INSPECTED AND TESTED FORWARD ENTRY DOOR IAW FAULT ISOLATION MANUAL 52-10-08. NO FAULTS FOUND. ACFT RELEASED FOR SERVICE. SUBSEQUENT FLIGHT REPORTED, N
- [SDR SROM0418201403](https://openairdocs.org/sdr/SROM0418201403.md): Intercostal · cracked · Apr 18, 2014 · N660CP · Boeing 7377BD · Fuselage Miscellaneous Structure
  > FOUND CRACK IN INTERCOSTAL NEXT TO FLOOR PANEL ATTACH NUTPLATE.
- [SDR SROM0418201402](https://openairdocs.org/sdr/SROM0418201402.md): Floor Panel · cracked · Apr 18, 2014 · N660CP · Boeing 7377BD · Fuselage Floor Panel
  > FLOOR PANEL FOUND CRACKED.
- [SDR SROM0418201401](https://openairdocs.org/sdr/SROM0418201401.md): Floor Panel · cracked · Apr 18, 2014 · N660CP · Boeing 7377BD · Fuselage Floor Panel
  > FLOOR PANEL FOUND CRACKED.
- [SDR SROM201311210001](https://openairdocs.org/sdr/SROM201311210001.md): Downlock Switch · out of tolerance · Nov 19, 2013 · N660CP · Boeing 7377BD · Landing Gear Position and Warning
  > DURING CLIMB OUT, AFTER GEAR RETRACTION, FORWARD PANEL GEAR INDICATOR SHOWED RT MAIN GEAR STILL DOWN AND LOCKED. OVERHEAD GEAR INDICATOR SHOWED ALL 3 GEAR UP AND LOCKED. RETURNED TO DEPARTURE. LANDED UNEVENTFUL. FOUND RT GEAR PRIMARY DOWN LOCK PROXIMITY SWI
- [SDR SROM2010017](https://openairdocs.org/sdr/SROM2010017.md): Compressor Blade · nicked · Dec 16, 2010 · N660CP · Boeing 7377BD · Turbine Engine Compressor Section
  > NR 2 ENG BIRD STRIKE AND INGESTION AT THE 9 O’CLOCK POSITION. BLOOD AND FEATHERS FOUND ON BLADES IN BYPASS PATH AND BOOSTER INLET. CONDITIONAL INSP COMPLIED WITH IAW AMM 05-51-18 AND 71-00-00. NO DEFECTS NOTED. ENGINE BORESCOPE INSP OF HIGH PRESSURE COMPRESS
- [SDR SROM20100001](https://openairdocs.org/sdr/SROM20100001.md): Autopilot Sys · disconnected · Feb 19, 2010 · N660CP · Boeing 7377BD · Autopilot System
  > SPEED TRIM FAIL LIGHT ILLUMINATED AND YAW DAMPER WON'T ENGAGE DURING TAKEOFF. MADE UNEVENTFUL RETURN TO DEPARTURE AIRPORT. PERFORMED YAW DAMPER SYS TEST IAW AMM 22-23-00, NO DEFECTS NOTED. PERFORMED DFCS BITE PROCEDURE AND DFCS ADJUSTMENT/TEST IAW AMM 22-11-
- [SDR SROM20090001](https://openairdocs.org/sdr/SROM20090001.md): Windshield · cracked · May 28, 2009 · N660CP · Boeing 7377BD · Flight Compartment Windows
  > MULTIPLE BIRD STRIKES ON DEPARTURE, RETURNED TO AIRPORT. REPLACED F/O WINDSHIELD. REPLACED 5 RIVETS UNDER INBD STRAFE OF NR 2 ENGINE NOSE COWL. CLEANED MULTIPLE BIRD REMAINS FROM RT FUSELAGE NOSE AND TAIL OF ACFT. PERFORMED BIRD STRIKE INSP IAW AMM 05-51-1

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N660CP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N660CP/reports

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